| Task |
KE-weapon system predominantly for anti tank application.
Apllication of technology to air-defence missile with dual pulse
motor and lateral thrust devices
|
| Customer |
BWB / BMVg
|
| Technology |
High performance composite propellant in light weight structure
(CFRP-Case).
Missile velocity > Mach 5
|
| Programme scope |
High performance composite propellant in light weight structure
(CFRP-Case).
Missile velocity > Mach 5
|
| Milestones |
Design, manufacturing and static tests 1990 -1993
First test flight 1993
Test flight with lateral thrust modules 1995, 1997 |
Hypervelocity motor thrust profile
|
Firing HFK 1
Hypervelocity experimental
missile 1st generation
|
